View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 49070U 26145.59599250 +.00000000 +00000-0 +12336-3 0 00003
2 49070 97.8927 220.6835 0001466 91.2288 268.9093 14.81673050 09
| Epoch (UTC): | 25 May 2026 14:18:13 |
| Eccentricity: | 0.0001466 |
| inclination: | 97.8927° |
| perigee height: | 623 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 220.6835° |
| argument of perigee: | 91.2288° |
| revolutions per day: | 14.81673050 |
| mean anomaly at epoch: | 268.9093° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|